Antenna integrated device and underwater apparatus
Patent Information
- Application Number
- CN202522290860.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-29
- Publication Date
- 2026-09-11
- Estimated Expiration
- 2035-10-29
AI Technical Summary
现有天线集成装置中用到的弯折后的射频线缆会增加射频路径长度,且增加插入损耗
本申请通过将第一卫星通信天线、第二卫星通信天线和无线电天线集成且沿水平方向同轴设置在第二壳体的第二容置腔内,并通过连接件内的连接线缆与第一壳体的通信模块连接,实现了多天线系统的紧凑布局,减少了设备体积和复杂度。另外,沿水平方向同轴设置的连接件、第一壳体和第二壳体避免了射频线缆的弯折,进而降低了射频损耗,提高了信号传输的稳定性。
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Figure CN224745875U_ABST
Abstract
Description
Technical Field
[0001] This application relates to the technical field of antennas, and more specifically, to an antenna integration device and underwater equipment. Background Technology
[0002] Underwater equipment (such as underwater robots) uses antenna integration devices for its communication equipment. Antenna integration devices refer to devices that integrate communication modules with antenna devices.
[0003] The inventors of this application have discovered that underwater equipment relying solely on satellite communication faces the risk of signal obstruction and communication interruption, while relying solely on radio communication carries the risk of communication interruption due to exceeding the effective signal coverage range or obstruction by obstacles. The bent RF cables used in existing antenna integration devices increase the RF path length and insertion loss. Furthermore, existing antenna integration devices are often complex in shape and occupy a large volume, which can increase drag if used in underwater robots.
[0004] The content in the background section is merely technology known to the public and does not necessarily represent existing technology in this field. Utility Model Content
[0005] This application aims to provide an antenna integration device and underwater equipment for at least one of the above-mentioned problems.
[0006] According to one aspect of this application, an antenna integration device is provided, including a first housing, a communication module, a second housing, a connector, and an antenna assembly. The first housing has a first receiving cavity. The communication module is disposed in the first receiving cavity. The second housing has a second receiving cavity. The connector houses a connecting cable, one end of which is connected to the first housing, and the other end is connected to the second housing. The connector, the first housing, and the second housing are coaxially arranged. The antenna assembly includes a first satellite communication antenna, a second satellite communication antenna, and a radio antenna. The first satellite communication antenna is disposed in the second receiving cavity and connected to the communication module via the connecting cable. The second satellite communication antenna is disposed in the second receiving cavity and connected to the communication module via the connecting cable. The radio antenna is disposed in the second receiving cavity and connected to the communication module via the connecting cable. The first satellite communication antenna, the second satellite communication antenna, and the radio antenna are coaxially arranged in the horizontal direction.
[0007] According to some embodiments of this application, the second housing has a club-shaped structure.
[0008] According to some embodiments of this application, the first satellite communication antenna is a Tiantong antenna, and the second satellite communication antenna is a Beidou antenna.
[0009] According to some embodiments of this application, the communication module includes a first satellite communication module, a second satellite communication module, and a radio communication module. The first satellite communication module is connected to a first satellite communication antenna via a Tiantong RF cable in a connecting cable. The second satellite communication module is connected to a second satellite communication antenna via a Beidou RF cable in a connecting cable. The radio communication module is connected to a radio antenna via a radio RF cable in a connecting cable.
[0010] According to some embodiments of this application, the first housing is provided with an external threaded interface for detachable connection with underwater equipment.
[0011] According to some embodiments of this application, the external threaded interface is provided with a sealing gasket and a waterproof and breathable valve.
[0012] According to some embodiments of this application, the connector is a straight rod-shaped structure, with both ends detachably connected to the first housing and the second housing respectively via metal threaded interfaces.
[0013] According to some embodiments of this application, the cross-sections perpendicular to the axial direction of the first housing, the connector, and the second housing are all circular. The diameter of the first housing is 80-90 mm and the length is 140-150 mm, the diameter of the connector is 15-20 mm and the length is 500-530 mm, and the diameter of the second housing is 30-40 mm and the length is 350-420 mm.
[0014] According to some embodiments of this application, the inner wall of the first housing is provided with a shock-absorbing pad.
[0015] According to some embodiments of this application, the first housing is provided with a watertight connector for detachable connection with underwater equipment.
[0016] According to another aspect of this application, an underwater device is also provided, including the antenna integration device described above.
[0017] Beneficial effects This application achieves a compact layout of a multi-antenna system by integrating a first satellite communication antenna, a second satellite communication antenna, and a radio antenna, and coaxially arranging them horizontally within a second accommodating cavity of a second housing. These antennas are then connected to the communication module of the first housing via connecting cables within a connector. This reduces the size and complexity of the device. Furthermore, the horizontally coaxial connector, the first housing, and the second housing prevent bending of the RF cables, thereby reducing RF loss and improving signal transmission stability. Attached Figure Description
[0018] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.
[0019] Figure 1 A schematic diagram of the appearance of an antenna integration device according to an embodiment of this application is shown; Figure 2 Another external schematic diagram of the antenna integration device according to an embodiment of this application is shown; Figure 3 A cross-sectional schematic diagram of an antenna integration device according to an embodiment of this application is shown.
[0020] Explanation of reference numerals in the attached figures: Antenna integration device 1; first housing 11; communication module 12; second housing 13; connector 14; antenna assembly 15; first accommodating cavity 111; first satellite communication module 121; second satellite communication module 122; radio communication module 123; second accommodating cavity 131; connecting cable 141; first satellite communication antenna 151; second satellite communication antenna 152; radio antenna 153; external thread interface 112; waterproof and breathable valve 1121; watertight connector 113. Detailed Implementation
[0021] Exemplary embodiments will now be described more fully with reference to the accompanying drawings. However, these exemplary embodiments can be implemented in many forms and should not be construed as limited to the embodiments set forth herein; rather, they are provided so that this application will be thorough and complete, and will fully convey the concept of the exemplary embodiments to those skilled in the art. The same reference numerals in the drawings denote the same or similar parts, and therefore repeated descriptions of them will be omitted.
[0022] The described features, structures, or characteristics can be combined in any suitable manner in one or more embodiments. Numerous specific details are provided in the following description to give a full understanding of embodiments of this disclosure. However, those skilled in the art will recognize that the technical solutions of this disclosure can be practiced without one or more of these specific details, or other methods, components, materials, devices, etc. In these cases, well-known structures, methods, devices, implementations, materials, or operations will not be shown or described in detail.
[0023] Furthermore, the terms “comprising” and “having”, and any variations thereof, are intended to cover non-exclusive inclusion. For example, a process, method, system, product, or apparatus that includes a series of steps or units is not limited to the steps or units listed, but may optionally include steps or units not listed, or may optionally include other steps or units inherent to such process, method, product, or apparatus.
[0024] The terms "first," "second," etc., in the specification, claims, and accompanying drawings of this application are used to distinguish different objects, rather than to describe a specific order.
[0025] The technical solutions of this application will be clearly and completely described below with reference to the accompanying drawings of the embodiments. The described embodiments are only some, not all, of the embodiments of this application. All other embodiments obtained by those skilled in the art based on the embodiments of this application without creative effort are within the scope of protection of this application.
[0026] According to one aspect of this application, an antenna integration device is provided. Figure 1 A schematic diagram of the appearance of an antenna integration device according to an embodiment of this application is shown. Figure 2 This illustration shows another external schematic diagram of the antenna integration device according to an embodiment of this application. Figure 3 A schematic cross-sectional view of an antenna integration device according to an embodiment of this application is shown. According to an example embodiment, such as... Figure 1 , Figure 2 and Figure 3 As shown, the antenna integration device 1 includes a first housing 11, a communication module 12, a second housing 13, a connector 14, and an antenna assembly 15. The first housing 11 has a first receiving cavity 111 inside. The communication module 12 is disposed in the first receiving cavity 111. The second housing 13 has a second receiving cavity 131 inside. The connector 14 houses a connecting cable 141, with one end connected to the first housing 11 and the other end connected to the second housing 13. The connector 14, the first housing 11, and the second housing 13 are coaxially arranged in the horizontal direction.
[0027] For example, the connecting cable 141 is an radio frequency connecting cable. For example, the connector 14, the first housing 11, and the second housing 13 are all cylinders.
[0028] Antenna assembly 15 includes a first satellite communication antenna 151, a second satellite communication antenna 152, and a radio antenna 153. The first satellite communication antenna 151 is disposed in the second accommodating cavity 131 and connected to the communication module 12 via a connecting cable 141. The second satellite communication antenna 152 is disposed in the second accommodating cavity 131 and connected to the communication module 12 via a connecting cable 141. The radio antenna 153 is disposed in the second accommodating cavity 131 and connected to the communication module 12 via a connecting cable 141. The first satellite communication antenna 151, the second satellite communication antenna 152, and the radio antenna 153 are coaxially arranged in the horizontal direction.
[0029] Through the above embodiments, this application achieves a compact layout of a multi-antenna system by integrating the first satellite communication antenna, the second satellite communication antenna, and the radio antenna and coaxially arranging them horizontally within the second accommodating cavity of the second housing, and connecting them to the communication module of the first housing via connecting cables within the connector. This reduces the size and complexity of the device. Furthermore, the horizontally coaxial connector, the first housing, and the second housing prevent bending of the RF cables, thereby reducing RF loss and improving the stability of signal transmission.
[0030] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the second shell 13 has a club-shaped structure.
[0031] Through the above embodiments, by defining the second housing as a club-shaped structure, this application can utilize the streamlined curve characteristics of the club-shaped structure to reduce the fluid resistance of the antenna integration device when used underwater.
[0032] According to the example embodiment, the first satellite communication antenna 151 is a Tiantong antenna and the second satellite communication antenna 152 is a Beidou antenna.
[0033] Through the above embodiments, this application improves the system robustness of the antenna integration device in complex underwater environments by defining the first satellite communication antenna and the second satellite communication antenna.
[0034] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3As shown, the communication module 12 includes a first satellite communication module 121, a second satellite communication module 122, and a radio communication module 123. The first satellite communication module 121 is connected to the first satellite communication antenna 151 via a Tiantong radio frequency cable (not shown) in the connecting cable 141. The second satellite communication module 122 is connected to the second satellite communication antenna 152 via a Beidou radio frequency cable (not shown) in the connecting cable 141. The radio communication module 123 is connected to the radio antenna 153 via a radio frequency cable (not shown) in the connecting cable 141.
[0035] Through the above embodiments, this application reduces signal crosstalk by connecting the first satellite communication module, the second satellite communication module, and the radio communication module to their respective antennas via corresponding RF cables. Furthermore, the coaxial layout shortens the RF path, reduces bending losses, and improves signal transmission efficiency.
[0036] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the first housing 11 is provided with an external threaded interface 112, which is used for detachable connection with underwater equipment (such as an underwater robot).
[0037] Through the above embodiments, this application achieves a detachable connection with underwater equipment (such as underwater robot equipment) by providing an external threaded interface in the first housing, thereby improving the efficiency of disassembly and assembly.
[0038] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the external threaded interface 112 is provided with a sealing gasket (not shown in the figure) and a waterproof and breathable valve 1121.
[0039] Through the above embodiments, this application improves the sealing performance of the external thread interface when connected to underwater equipment (such as an underwater robot) by setting a sealing gasket and a waterproof and breathable valve at the external thread interface, and avoids leakage of the first housing due to pressure changes.
[0040] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the connector 14 is a straight rod structure, and its two ends are detachably connected to the first housing 11 and the second housing 13 respectively through metal threaded interfaces (not shown in the figure).
[0041] Through the above embodiments, this application improves assembly and disassembly efficiency by providing metal threaded interfaces at both ends of the straight rod-shaped connector, enabling rapid assembly and disassembly of the first and second housings. Furthermore, the threaded connection allows for partial replacement of damaged components (such as replacing the connecting rod or housing) without requiring overall disassembly, thus reducing maintenance costs.
[0042] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the cross-sections perpendicular to the axial direction of the first housing 11, the connector 14, and the second housing 13 are all circular. The diameter of the first housing is 80-90 mm and the length is 140-150 mm, the diameter of the connector is 15-20 mm and the length is 500-530 mm, and the diameter of the second housing is 30-40 mm and the length is 350-420 mm.
[0043] For example, the first housing 11 has a diameter of 85.5 mm and a length of 144.73 mm, the connector 14 has a diameter of 18 mm and a length of 526.5 mm, and the second housing 13 has a diameter of 35 mm and a length of 400.4 mm.
[0044] Through the above embodiments, this application reduces the overall size of the antenna integration device and improves its portability by setting the specific dimensions of the first housing, the connector, and the second housing.
[0045] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the inner wall of the first housing 11 is provided with a shock-absorbing pad (not shown in the figure).
[0046] Through the above embodiments, this application reduces the vibration and impact on the communication module disposed inside the first accommodating cavity by providing a shock-absorbing pad inside the first housing, thereby improving the stability of the antenna integration device.
[0047] According to the example embodiment, such as Figure 1 , Figure 2 and Figure 3 As shown, the first housing 11 is provided with a watertight connector 113, which is used for detachable connection with underwater equipment (such as an underwater robot).
[0048] Through the above embodiments, this application improves the sealing performance of the connection between the antenna integration device and the underwater equipment by providing a watertight connector in the first housing to connect the underwater equipment (such as an underwater robot).
[0049] According to another aspect of this application, an underwater device is also provided, including the antenna integration device described above.
[0050] Finally, it should be noted that the above description is merely a preferred embodiment of this application and is not intended to limit this application. Although this application has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions of the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the protection scope of this application.
Claims
1. An antenna integration device for underwater equipment, characterized in that, include: The first housing has a first receiving cavity inside; A communication module is disposed in the first accommodating cavity; The second housing has a second accommodating cavity inside; A connector internally houses a connecting cable. One end of the connector is connected to the first housing, and the other end is connected to the second housing. The connector, the first housing, and the second housing are coaxially arranged in the horizontal direction. Antenna assembly, including: A first satellite communication antenna is disposed in the second accommodating cavity and connected to the communication module via the connecting cable; A second satellite communication antenna is disposed in the second accommodating cavity and connected to the communication module via the connecting cable; A radio antenna is disposed in the second accommodating cavity and connected to the communication module via the connecting cable; The first satellite communication antenna, the second satellite communication antenna, and the radio antenna are arranged coaxially in the horizontal direction.
2. The antenna integration device according to claim 1, characterized in that, The second shell has a pestle-shaped structure.
3. The antenna integration device according to claim 1, characterized in that, The first satellite communication antenna is a Tiantong antenna, and the second satellite communication antenna is a Beidou antenna.
4. The antenna integration device according to claim 1 or 2, characterized in that, The communication module includes: The first satellite communication module is connected to the first satellite communication antenna via the Tiantong radio frequency cable in the connecting cable; The second satellite communication module is connected to the second satellite communication antenna via the BeiDou radio frequency cable in the connecting cable; The radio communication module is connected to the radio antenna via a radio frequency cable in the connecting cable.
5. The antenna integration device according to claim 1, characterized in that, The first housing is provided with an external threaded interface, which is used for detachable connection with the underwater equipment.
6. The antenna integration device according to claim 5, characterized in that, The external threaded interface is equipped with a sealing gasket and a waterproof and breathable valve.
7. The antenna integration device according to claim 1, characterized in that, The connector is a straight rod-shaped structure, with both ends detachably connected to the first housing and the second housing respectively via metal threaded interfaces.
8. The antenna integration device according to claim 1, characterized in that, The cross-sections perpendicular to the axial direction of the first housing, the connecting member, and the second housing are all circular. The first housing has a diameter of 80-90mm and a length of 140-150mm, the connector has a diameter of 15-20mm and a length of 500-530mm, and the second housing has a diameter of 30-40mm and a length of 350-420mm.
9. The antenna integration device according to claim 1, characterized in that, The first housing is provided with a watertight connector, which is used for detachable connection with the underwater equipment.
10. An underwater device, characterized in that, The underwater device includes the antenna integration device as described in any one of claims 1-9.